Fixed wing
UAVDB Sport Cub S2
Fixed-wing flight dynamics and system identification
Piloted Sport Cub S2 maneuver segments for flight-dynamics analysis, with inertial/GPS state, control commands and propulsion telemetry.
Access links
Primary places to inspect, download, read about, or reproduce the dataset.
Quick facts
- Vehicle type
- Fixed wing
- Environment
- Outdoor
- Data origin
- Real-world
- Sensor count
- 3
- Ground truth
- Not reported
- Calibration
- Not reported
- Annotations
- Not reported
Sensor overview
High-level sensor availability before the detailed sensor records below.
Ground truth
Reference scope, method, rate, coverage, and provenance.
Not reported
Calibration and synchronization
Reported calibration level, reproducibility signals, and supporting notes.
- Level
- Not reported
- Processed parameters
- Not reported
- Raw calibration data
- Not reported
- Calibration targets
- Not reported
Calibration data
Calibration reproducibility details are not reported.
Notes
No dedicated released raw sensor-calibration package or reference-trajectory accuracy is established by this paper. Aircraft geometry, aerodynamic tests and command trim are not interchangeable with sensor calibration.
Known or intentional limitations
Reported constraints and characteristics to check before using the dataset.
Released maneuver segments are selected and filtered rather than a complete unfiltered flight campaign.
Flight count is approximate and is not the number of released maneuver segments.
The paper Pitot-installation prose is inconsistent with its equipment table and later airspeed plots.
The release does not establish an independent pose ground-truth trajectory.
All 53 current maneuver files contain airspeed values, with missing samples and complex-valued airspeed in four files. The 400 Hz acquisition grid does not establish a pitot rate. The pressure channel is not verified as differential pressure. Official documentation confirms installation despite the paper’s future-tense sentence.
Cameras
Not reported
IMUs
Al Volo inertial measurements
- Model
- XSens MTi-G-700
- Count
- 1
- Accel / gyro
- Not reported
GNSS
XSens MTi-G-700
- Model or name
- XSens MTi-G-700
- Count
- 1
- Rate
- Not reported
- GNSS type
- GPS_IMU
- Position output
- Available
- Velocity output
- Available
- Heading output
- Not reported
LiDAR
Not reported
Radar
Not reported
Pitot tube
Al Volo Pitot Static Airspeed Sensor
- Model or name
- Al Volo Pitot Static Airspeed Sensor
- Count
- Not reported
- Rate
- Not reported
- Airspeed output
- Available (m/s)
- Differential pressure
- Not reported
- Notes
- All 53 current maneuver files contain airspeed values, with missing samples and complex-valued airspeed in four files. The 400 Hz acquisition grid does not establish a pitot rate. The pressure channel is not verified as differential pressure. Official documentation confirms installation despite the paper’s future-tense sentence.
Additional sensors
Magnetometer
- Name
- Integrated magnetic-field measurements
- Count
- 1
- Notes
- Three-axis magnetic field is part of the same nine-axis unit; no separate chip model or native rate is established.
Annotations
Reported annotation availability and task support.
- Availability
- Not reported
- Format
- Not reported
- Class count
- Not reported
Semantic segmentation
Not reported
Instance segmentation
Not reported
Object detection
Not reported
Optical flow
Not reported
Depth ground truth
Not reported
Citation
Citation key and BibTeX kept at the end of the page for reference.
@inproceedings{dantsker2019sportcub,
title = {Flight & Ground Testing Data Set for Subscale GA Aircraft: 26%-scale Cub Crafters CC11-100 Sport Cub S2},
author = {Dantsker, Or D. and Vahora, Moiz and Mancuso, Renato},
year = {2019},
booktitle = {AIAA Scitech 2019 Forum},
doi = {10.2514/6.2019-1616},
}Dataset corrections
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